This paper presents a generalization of the divide and conquer algorithm for sensitivity analysis of dynamic multibody systems based on direct differentiation. While similar sensitivity analysis approach has been demonstrated for multi-rigid and multi-flexible systems in tree topologies and a limited set of kinematically closed loop topologies, this paper presents the generalization of these approaches to systems in generalized topologies including many coupled kinematically closed loops. This generalization retains the efficient complexity of the underlying formulations i.e. linear and logarithmic complexity in serial and parallel implementation. Other than the computational efficiency, the advantages of this method include concurrent sensitivity analysis with forward dynamics, no numerical artifacts arising from parametric perturbation and significantly reduced data storage compared to traditional methods. An interesting application of this work in control of multibody systems is discussed.
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ASME 2011 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference
August 28–31, 2011
Washington, DC, USA
Conference Sponsors:
- Design Engineering Division and Computers and Information in Engineering Division
ISBN:
978-0-7918-5481-5
PROCEEDINGS PAPER
Efficient Operational Space Sensitivity Analysis of Dynamic Multibody Systems Available to Purchase
Rudranarayan M. Mukherjee
Rudranarayan M. Mukherjee
NASA Jet Propulsion Laboratory - California Institute of Technology, Pasadena, CA
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Rudranarayan M. Mukherjee
NASA Jet Propulsion Laboratory - California Institute of Technology, Pasadena, CA
Paper No:
DETC2011-48884, pp. 403-410; 8 pages
Published Online:
June 12, 2012
Citation
Mukherjee, RM. "Efficient Operational Space Sensitivity Analysis of Dynamic Multibody Systems." Proceedings of the ASME 2011 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. Volume 4: 8th International Conference on Multibody Systems, Nonlinear Dynamics, and Control, Parts A and B. Washington, DC, USA. August 28–31, 2011. pp. 403-410. ASME. https://doi.org/10.1115/DETC2011-48884
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